COMPLIANCES IN A TURBOMACHINE WITH A SPEED REDUCER
Disclosed is an assembly for a turbomachine, comprising: *-a first connection element (9) having a first radial compliance (SRI); *-a second connection element (10) having a second radial compliance (SR2); *-a third connection element (11) having a third radial compliance (SR3); and *-a fourth conne...
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| creator | TAN-KIM, Alexandre Jean-Marie GIVERT, Maxime Paul Numa BECOULET, Julien Fabien Patrick |
| description | Disclosed is an assembly for a turbomachine, comprising: *-a first connection element (9) having a first radial compliance (SRI); *-a second connection element (10) having a second radial compliance (SR2); *-a third connection element (11) having a third radial compliance (SR3); and *-a fourth connection element (12) having a fourth radial compliance (SR4), wherein a ratio of the first radial compliance (SRI) to the third radial compliance (SR3) is strictly lower than 10%, and/or a ratio of the first radial compliance (SRI) to the second radial compliance (SR2) is strictly lower than 4%, and/or a ratio of the first radial compliance (SRI) to the fourth radial compliance (SR4) is strictly lower than 50%. |
| format | Patent |
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*-a second connection element (10) having a second radial compliance (SR2); *-a third connection element (11) having a third radial compliance (SR3); and *-a fourth connection element (12) having a fourth radial compliance (SR4), wherein a ratio of the first radial compliance (SRI) to the third radial compliance (SR3) is strictly lower than 10%, and/or a ratio of the first radial compliance (SRI) to the second radial compliance (SR2) is strictly lower than 4%, and/or a ratio of the first radial compliance (SRI) to the fourth radial compliance (SR4) is strictly lower than 50%.</description><language>eng ; fre ; ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2024</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240717&DB=EPODOC&CC=EP&NR=4399401A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20240717&DB=EPODOC&CC=EP&NR=4399401A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TAN-KIM, Alexandre Jean-Marie</creatorcontrib><creatorcontrib>GIVERT, Maxime Paul Numa</creatorcontrib><creatorcontrib>BECOULET, Julien Fabien Patrick</creatorcontrib><title>COMPLIANCES IN A TURBOMACHINE WITH A SPEED REDUCER</title><description>Disclosed is an assembly for a turbomachine, comprising: *-a first connection element (9) having a first radial compliance (SRI); 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GIVERT, Maxime Paul Numa ; BECOULET, Julien Fabien Patrick</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4399401A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2024</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>TAN-KIM, Alexandre Jean-Marie</creatorcontrib><creatorcontrib>GIVERT, Maxime Paul Numa</creatorcontrib><creatorcontrib>BECOULET, Julien Fabien Patrick</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TAN-KIM, Alexandre Jean-Marie</au><au>GIVERT, Maxime Paul Numa</au><au>BECOULET, Julien Fabien Patrick</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>COMPLIANCES IN A TURBOMACHINE WITH A SPEED REDUCER</title><date>2024-07-17</date><risdate>2024</risdate><abstract>Disclosed is an assembly for a turbomachine, comprising: *-a first connection element (9) having a first radial compliance (SRI); *-a second connection element (10) having a second radial compliance (SR2); *-a third connection element (11) having a third radial compliance (SR3); and *-a fourth connection element (12) having a fourth radial compliance (SR4), wherein a ratio of the first radial compliance (SRI) to the third radial compliance (SR3) is strictly lower than 10%, and/or a ratio of the first radial compliance (SRI) to the second radial compliance (SR2) is strictly lower than 4%, and/or a ratio of the first radial compliance (SRI) to the fourth radial compliance (SR4) is strictly lower than 50%.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
| title | COMPLIANCES IN A TURBOMACHINE WITH A SPEED REDUCER |
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